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I'm planning on running a series of tests with a number of different spacecraft, mostly capsules, to see how they behave with different reentry conditions.
While I can directly figure out most things like the reentry angle and speed at entry interface, I'm not sure how to determine the reentry anticipation from the spacecraft's position at entry interface and ultimate landing site.
Any thoughts on this matter?
While I can directly figure out most things like the reentry angle and speed at entry interface, I'm not sure how to determine the reentry anticipation from the spacecraft's position at entry interface and ultimate landing site.
Any thoughts on this matter?